Daniel Macinnis resumes & CV records
Resumes
Aerospace Engineering Manager At Raytheon Missile Systems
Location:
Tucson, Arizona Area
Industry:
Defense & Space
Daniel Vincent Macinnis, 60Santa Rita, AZ
Daniel Macinnis Phones & Addresses
Vail, AZ
Tucson, AZ
114 Chardonnay Ln, Tolland, CT 06084 860-8710933 860-9569768
Kingsville, TX
Indianapolis, IN
San Diego, CA
Pima, AZ
114 Chardonnay Ln, Tolland, CT 06084 860-5757130
Social networks
Daniel Vincent Macinnis
Linkedin
Work
Position:
Administrative Support Occupations, Including Clerical Occupations
Education
Degree:
High school graduate or higher
Emails
Industries
Defense & Space
Mentions for Daniel Vincent Macinnis
Publications & IP owners
Us Patents
Rocket Multi-Nozzle Grid Assembly And Methods For Maintaining Pressure And Thrust Profiles With The Same
US Patent:
2012023, Sep 20, 2012
Filed:
Mar 16, 2011
Appl. No.:
13/049024
Inventors:
Daniel Chasman - Tucson AZ, US
Stephen D. Haight - Oro Valley AZ, US
Daniel V. MacInnis - Vail AZ, US
Stephen D. Haight - Oro Valley AZ, US
Daniel V. MacInnis - Vail AZ, US
Assignee:
Raytheon Company - Waltham MA
International Classification:
F02K 9/97
B23P 11/00
B23P 11/00
US Classification:
60204, 60263, 29888
Abstract:
A rocket multi-nozzle grid assembly includes an insulator grid, a plurality of refractory nozzle fittings and a grid support plate. The grid support plate braces the plurality of refractory nozzle fittings and the insulator grid. The insulator grid includes insulator orifices, each of the nozzle fittings includes a fitting orifice and the grid support plate includes a plurality of plate orifices. The rocket multi-nozzle grid assembly includes a plurality nozzles. Each nozzle includes a plate orifice aligned with one insulator orifice and one fitting orifice. Exhaust gases are directed through the plurality of nozzles. The multi-nozzle grid assembly substantially maintains its surface area throughout operation of a rocket motor. In one example, the surface area is maintained through ablation of the insulator grid. In another example, the surface area is maintained through cooling of the plurality of nozzle fittings with the ablated fragments passing through the nozzles.
Electrically Operated Pulse Initiators And Ignition
US Patent:
2017009, Apr 6, 2017
Filed:
Oct 6, 2015
Appl. No.:
14/875741
Inventors:
- Waltham MA, US
Mark T. Langhenry - Tucson AZ, US
Matt H. Summers - Marana AZ, US
Daniel V. Macinnis - Vail AZ, US
Mark T. Langhenry - Tucson AZ, US
Matt H. Summers - Marana AZ, US
Daniel V. Macinnis - Vail AZ, US
International Classification:
F42B 3/04
Abstract:
A gas generation system for generating gases, such as for use as or as part of a rocket motor in propelling a projectile, includes two or more propellant charges and electrically operated propellant initiators operatively coupled to respective of the propellant charges, to initiate combustion in the propellant charges, wherein the propellant charges are operatively isolated from one another such that the propellant charges can be individually initiated and are not ignited due to gases generated from other of the propellant charges being combusted.
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